Aircraft Structure Reinforcement Using Segmented Dual-Strap System

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Solution Overview

Problem

Aircraft structures require reinforcement during retrofit or repair procedures, but existing methods using high-strength steel reinforcing straps are prone to low toughness and rapid crack propagation, leading to increased maintenance frequency and downtime.

Innovation Solution

The use of a dual-layer reinforcing strap system, where a first strap is attached to the structural component and a second strap is attached to the first strap, providing redundancy and allowing for crack detection during inspection without compromising load capacity, with the second strap being thicker and taller than the first to ensure visibility and maintain structural integrity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a single reinforcing strap is used to reinforce the structural component, then the reinforcement provides sufficient load capacity, but a crack in the strap can propagate rapidly due to low toughness of high-strength steel material

Engineering Contradiction:
Improveload capacityVSAvoidcrack propagation resistance
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The single reinforcing strap is divided into multiple separate straps (first reinforcing strap and second reinforcing strap) that are attached in sequence. This segmentation ensures that a crack in one strap cannot propagate into the other straps, providing independent crack containment while maintaining the required load capacity through the combined strength of multiple straps.

Inventive Principle:
Principle #1Segmentation

2Volume of moving object

If high-strength steel material is used for the reinforcing strap, then the strap size is reduced for the same load, but the toughness is low leading to rapid crack propagation

Engineering Contradiction:
Improvestrap sizeVSAvoidtoughness
Core Design Contradiction:
Volume of moving objectVSReliability

Solution Approach 1:

The high-strength steel reinforcement is segmented into multiple straps, allowing the use of high-strength material (for compact size) while the segmentation itself provides crack propagation resistance. The multiple straps work together to maintain the required strength while preventing catastrophic failure from a single crack.

Inventive Principle:
Principle #1Segmentation

3Reliability

If multiple reinforcing straps are used to provide redundancy and prevent crack propagation, then the reliability is improved, but the device complexity increases

Engineering Contradiction:
Improvecrack propagation resistanceVSAvoidnumber of straps
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The reinforcement system is segmented into a specific number of straps (at least two) attached in sequence, providing the necessary redundancy and crack propagation resistance. This segmented approach achieves improved reliability while keeping the complexity manageable through a systematic arrangement of multiple identical components.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS9810601B2Aircraft structure
Publication Date: 2017.11.07 AIRBUS OPERATIONS LTD
  • US9810601B2 patent drawing
  • US9810601B2 patent drawing
  • US9810601B2 patent drawing

AI summary

The present invention provides an aircraft structure comprising a structural component and a set of reinforcing straps for reinforcing the structural component, wherein the set comprises a first reinforcing strap having an inner and outer surface, wherein the inner surface is attached to a first surface of the structural component such that the first reinforcing strap extends longitudinally along the structural component and a second reinforcing strap having an inner and outer surface, wherein the inner surface is attached to the outer surface of the first reinforcing strap such that the second reinforcing strap extends longitudinally along the first reinforcing strap. The invention also provides an aircraft, a method of reinforcing an aircraft structure and a method of inspecting an aircraft structure.